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Wikipedia / Hydra 70

The Hydra 70 rocket is an American made diameter fin-stabilized unguided rocket used primarily in the air-to-ground role. It can be equipped with a variety of warheads, and in more recent versions, guidance systems for point attacks. The Hydra is widely used by US and allied forces, competing with the Canadian CRV7, with which it is physically interchangeable.

Overview

The Hydra 70 is derived from the diameter Mk 4/Mk 40 Folding-Fin Aerial Rocket developed by the United States Navy for use as a free-flight aerial rocket in the late 1940s. The Mk40 was used during the Korean and Vietnam wars to provide close air support to ground forces from about 20 different firing platforms, both fixed-wing and armed helicopters.

The main change made to produce the Hydra was the Mk. 66 motor which uses a new propellant that offers considerably more thrust, (Mod 2/3) (Mod 4). The fins of the Mk 40 flipped forward from the rear when the rocket left the launching tube, but in the Hydra they are curved to match the outside diameter of the rocket fuselage and flip sideways to open, which is referred to as WAFAR (Wrap-Around Fin Aerial Rocket) instead of FFAR (folding-fin aerial rocket). To improve stability during the time the fins are still opening, the four motor nozzles have a slight cant angle to impart a spin while the rocket is still in the launch tube.

Today, the OH-58D(R) Kiowa Warrior, the Black Hawk, and AH-64E Apache Longbow, as well as the Marine Corps' versatile UH-1 Huey and AH-1 Cobra, carry the Hydra rocket launcher standard on its weapon pylons.

Mk 66 rocket motor variants

Designation

Description

Mk 66 Mod 0

70mm (2.75in) WAFAR universal motor; common motor for the GD Hydra 70 series of rockets; original prototype; for US Army. Introduced in 1972.

Mk 66 Mod 1

Mk 66 variant; production variant; for US Army

Mk 66 Mod 2

Mk 66 Mod 1 variant; HERO (Hazards of Electromagnetic Radiation to Ordnance) safe; for US Navy and US Air Force. Began production in 1986.

Mk 66 Mod 3

Mk 66 Mod 1 variant; HERO safe; Mk 66 Mod 2 for US Army

Mk 66 Mod 4

Mk 66 Mod 2/3 variant; incorporates a Salt rod to reduce exhaust gases; for all services. Began production in 1999.

Mk 66 Mod 5

Mk 66 Mod 4 variant; Incorporates propellant venting during fast cook off

Mk 66 Mod 6

Mk 66 Mod 4/5 variant; designed to reduce the tendency of secondary launch gases to combust in the parent aircraft’s engine, primarily with the AH-64 helicopter

Service

The family of Hydra 70 (70mm) 2.75inch rockets perform a variety of functions. The war reserve unitary and cargo warheads are used for anti-materiel, anti-personnel, and suppression missions. The Hydra 70 family of folding-fin aerial rockets also includes smoke screening, illumination, and training warheads. Hydra 70 rockets are known mainly by either their warhead type or by the rocket motor designation, Mk 66 in US military service.

United States

In the U.S. Army, Hydra 70 rockets are fired from the AH-64 Apache and AH-64D Apache Longbow helicopter variants using M261 19-tube rocket launchers, and the OH-58D Kiowa Warrior using seven-tube M260 rocket launchers. In the U.S. Marine Corps, either the M260 or M261 launchers are employed on the AH-1W SuperCobra and AH-1Z Viper, depending upon the mission. The M260 and M261 are used with the Mk 66 series of rocket motor, which replaced the Mk 40 series. The Mk 66 has a reduced system weight and provides a remote fuze setting interface. Hydra 70s have also been fired from UH-60 and AH-6 series aircraft in US Army service.

The AH-1G Cobra and the UH-1B "Huey" used a variety of launchers including the M158 seven-tube and M200 19-tube rocket launchers designed for the Mk 40 rocket motor; however, these models have been replaced by upgraded variants in the U.S. Marine Corps because they were not compatible with the Mk 66 rocket motor. The Hydra 70 rocket system is also used by the U.S. Navy and the U.S. Air Force.

Common U.S. Mk 66 compatible launchers

Designation

Description

M260

7-Tube LWL (LightWeight Launcher, 35 lbs, 15.9kg)

M261

19-Tube LWL (LightWeight Launcher, 80 lbs/ 36.3kg)

LAU-130/A

19-Tube rocket launcher

LAU-131/A

7-Tube rocket launcher

LAU-68D/A

7-Tube LAU-68C/A variant; compatible w/ Mk 66 rocket motor; external thermal protection coating; launcher supports single and ripple firing

LAU-69D/A

19-Tube LAU-61B/A variant; compatible w/ Mk 66 rocket motor; external thermal protection coating; launcher supports single and ripple firing

Accidents

In 2019, a 72-year-old Taiwanese man was killed after a discarded Hydra rocket which he had cut into with an electric saw exploded. He had believed it to be a length of pipe. The rocket had been caught in the net of a fishing vessel and then discarded by the crew ashore as scrap metal.

Warheads

Hydra 70 warheads fall into three categories:

  • Unitary warheads with impact-detonating fuzes or remote-set multi-option fuzes.

  • Cargo warheads with air burst-range, with settable fuzes using the "wall-in-space" concept or fixed standoff fuzes.

  • Training warheads.

Fuzing options

#

Designation

Description

Arming Range, Acceleration or Time

1

M423

Nose Mount, Point Detonating for slow speed platforms (helicopters)

2

M427

Nose Mount, Point Detonating for high speed platforms

3

XM436

Air burst, Motor-Burnout Delay

4

XM438/M438

Nose Mount, Point Detonating

5

M440

Point Detonating

6

Mk 352 Mod 0/1/2

Point Detonating

7

M429

Proximity Air burst

8

M433

Nose Mount, Resistance Capacitance (RC)

SuperQuick (PD) Delay in increments including Bunker penetrating option

9

M439

Base Mount, Resistance Capacitance (RC), Payload Discharging Pilot-Selectable

Discharges submunitions between ( on AH-1s) 27Gs

10

M442

Air burst, Motor-Burnout Delay

Discharges Flare at , 17-22 g required for arming

11

M446

Base Mount, Air burst, Motor-Burnout Delay

12

Model 113A

Base Mount, Air burst, Motor-Burnout Delay

Common warheads

The most common warhead for the Hydra 70 rocket is the M151 "10-Pounder," which has a blast radius of 10 meters and lethal fragmentation radius of around 50 meters. The M247 HEDP warheads have similar penetration to the standard M72 LAW warhead (~300 mm of rolled homogenous armor).

Designation

Description

Weight

Payload

Fuze Type

Fuzing options

M151

High explosive (HEDP) '10 pounder'

(w/o Fuze)

Comp B-4 HE

M423

1,2,5,7,8

M156

White phosphorus munitions (WP)

WP

M423 M429

1,2,6,7

M229

High explosive (HEDP); elongated M151 '17 pounder'

(Fuzed)

Comp B-4 HE

M423

1,2,6,7

M247

High-explosive anti-tank (HEAT)/high-explosive dual purpose (HEDP)

Comp B HE

M438 PD

4 (integral to warhead)

M255

APERS (anti-personnel) warhead

2500 flechettes

9

M255E1/A1

Flechette warhead

1179 flechettes

M439

9

M257

Parachute illumination

One M257 Candle (Flare) 1 million candela

M442

10 (integral to warhead)

M259

White phosphorus (WP)

9

M261

Multi-purpose submunition (MPSM)

9 M73 (Grenade) Submunitions

M439 with M84 electric detonator

9

M264

Red phosphorus (RP) Smoke

72 RP Pellets

M439

9

M267

MPSM Practice

Three Marking SMs, 6 Metal Weights

M439 with M84 electric detonator

9

M274

Practice (Smoke)

of potassium perchlorate and aluminum powder

M423

1

M278

Infra-red (IR) parachute illumination

One M278 IR Flare

M442

10 (integral to warhead)

M282

Multipurpose penetrator warhead

PBXN-110

delayed

Mk 67 Mod 0

White phosphorus (WP)

1,2,6,7

Mk 67 Mod 1

Red phosphorus (RP)

1,2,6,7

WTU-1/B

Practice

Inert

None

None

WDU-4/A

APERS warhead

96 flechettes of unknown weight

12 (integral to warhead)

WDU-4A/A

APERS warhead

2205 flechettes

M405A2

12 (integral to warhead)

Mk 66 rocket motor technical data

  • Weight:

  • Length:

  • Burn time: 1.07 sec

Average thrust ():

  • (Mod 2/3)

  • (Mod 4)

  • Motor burnout range:

  • Motor burnout velocity:

  • Launch spin rate: 10 rps, 35 rps after exiting launcher

  • Velocity at launcher exit:

Acceleration:

  • 60–70 g (initial)

  • 95–100 g (final)

  • Effective Range: depending on warhead and launch platform

  • Maximum Range: under optimum conditions

Precision guided Hydra 70

There are several design efforts to turn the Hydra 70 rocket into a precision guided munition (PGM) to produce a weapon with greater accuracy but at less cost than other guided missiles. These include:

The APKWS was the first to be fielded in March 2012, and the TALON entered full rate production for the United Arab Emirates Armed Forces in September 2014.

The Turkish ROKETSAN Cirit is a similar missile compatible with 70mm rocket launchers, but it was developed from scratch and does not use Hydra 70 components.

Operators

  • − APKWS

  • − Used on Bell OH-58D Kiowa helicopters

  • − APKWS

  • − APKWS

  • − APKWS

  • − APKWS

  • − APKWS

  • − APKWS

  • − APKWS

  • − APKWS

  • − APKWS

  • − Used on Mi-24 gunships

See also

Comparable weapon systems

Other

Bibliography

References

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